Patents for F23R 3 - Continuous combustion chambers using liquid or gaseous fuel (14,092) |
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11/02/1989 | DE3913223A1 Vorrichtung zum staendigen halten der ringfoermigen auslassmuendung des gasausstroemraums zentriert um die duesenanordnung in einer gasturbine Apparatus for continuously keep the exhaust port of the annular loop gasausstroemraums centered around the duesenanordnung in a gas turbine |
10/24/1989 | US4875339 Combustion chamber liner insert |
10/19/1989 | DE3906580A1 Lightweight turbojet (jet turbine) engine according to the principle of modular (unitised) construction |
10/12/1989 | DE3811293A1 Combustion chamber of a gas turbine |
10/11/1989 | EP0335978A1 Gas turbine combustor |
10/11/1989 | CN1036245A Wall having cooling passage |
10/11/1989 | CN1005423B High reliability fuel oil nozzle for a gas turbine |
10/10/1989 | US4872312 Gas turbine combustion apparatus |
10/04/1989 | EP0335481A1 Wall having cooling passage |
10/03/1989 | US4870826 Casing for a turbojet engine combustion chamber |
10/03/1989 | US4870825 Rotary fuel injection system |
10/03/1989 | US4870824 Passively cooled catalytic combustor for a stationary combustion turbine |
10/03/1989 | US4870818 Fuel nozzle guide structure and retainer for a gas turbine engine |
09/26/1989 | US4869062 Burner for solid and other high ash fuels |
09/26/1989 | CA1259778A1 Clip attachment |
09/20/1989 | EP0333307A1 Gas turbine combustor |
09/12/1989 | US4864828 Aircraft engine combustion liner cooling apparatus |
09/12/1989 | US4864827 Combustor |
09/12/1989 | US4864818 Augmentor liner construction |
09/12/1989 | CA1259197A1 High reliability fuel oil nozzle for a gas turbine |
09/05/1989 | US4863105 High reliability fuel oil nozzle for a gas turbine |
08/23/1989 | EP0328813A1 Flame holder mount for gas turbine engine |
08/17/1989 | DE3901233A1 Burner for a gas-turbine engine (power plant) |
08/17/1989 | DE3901232A1 Burner for a gas-turbine engine (power plant) |
08/15/1989 | US4857499 Platinum and palladium with promoters on porous support |
08/15/1989 | CA1258379A1 Gas turbine combustor |
08/08/1989 | US4854127 Bimodal swirler injector for a gas turbine combustor |
08/02/1989 | EP0326448A1 Mixing device with a variable section for the different jets of a jet engine |
08/01/1989 | US4852355 Dispensing arrangement for pressurized air |
08/01/1989 | CA1257972A1 Sliding joint for an annular combustor |
07/26/1989 | EP0204988B1 Flame tube |
07/26/1989 | CN1034259A Bimodal swirler injector for gas turbine combustor |
07/25/1989 | US4850194 Burner system |
07/18/1989 | US4848089 Combustor attachment device |
07/13/1989 | WO1989006309A1 Turbine combustor with tangential fuel injection and bender jets |
07/13/1989 | WO1989006308A1 Annular combustor with tangential cooling air injection |
07/13/1989 | WO1989006307A1 Gas turbine with forced vortex fuel injection |
07/11/1989 | US4845952 Multiple venturi tube gas fuel injector for catalytic combustor |
07/11/1989 | US4845940 Low NOx rich-lean combustor especially useful in gas turbines |
07/04/1989 | US4843825 Combustor dome heat shield |
07/04/1989 | CA1256708A1 Gas turbine engine augmentor |
06/29/1989 | WO1989005903A1 Fuel injectors for turbine engines |
06/28/1989 | EP0321809A1 Process for combustion of liquid fuel in a burner |
06/27/1989 | US4842197 Fuel injection apparatus and associated method |
06/27/1989 | US4841725 Fuel spray device for gas turbine augmentor or afterburner |
06/21/1989 | EP0321320A1 Turbine combustion chamber having a double-walled connection part |
06/21/1989 | EP0320746A1 Gas turbine plant |
06/13/1989 | US4838044 Warp-knit tape for hook-and-loop fasteners |
06/13/1989 | US4838031 Internally cooled combustion chamber liner |
06/13/1989 | US4838030 Combustion chamber liner having failure activated cooling and dectection system |
06/13/1989 | US4838029 Externally vaporizing system for turbine combustor |
06/07/1989 | EP0319246A2 Emissions control for gas turbine engine |
06/07/1989 | EP0318706A1 Water spray ejector system for steam injected engine |
06/06/1989 | US4835962 Fuel atomization apparatus for gas turbine engine |
06/06/1989 | US4835959 Multiple-propellant air vehicle and propulsion system |
05/31/1989 | EP0318312A1 Aperture insert for the combustion chamber of a gas turbine |
05/31/1989 | CN2038600U Distributor for jetling coal dust into blast |
05/30/1989 | US4833881 Gas turbine engine augmentor |
05/30/1989 | US4833878 Wide range gaseous fuel combustion system for gas turbine engines |
05/23/1989 | US4832999 Honeycomb structure assemblies |
05/17/1989 | EP0316233A1 Assembly method for two parts having different thermal expansion coefficients |
05/16/1989 | US4829764 Combustion air flow rate adjusting device for gas turbine combustor |
05/10/1989 | EP0315486A2 Aircraft engine frame construction |
05/10/1989 | EP0315485A2 Gas-cooled flameholder assembly |
05/10/1989 | EP0314977A2 Device for producing energy |
05/09/1989 | US4828441 Locked threaded insert for high stress application |
05/09/1989 | US4827724 Gas turbine combustion chamber |
05/03/1989 | EP0314261A1 Honeycomb structure assemblies |
05/03/1989 | EP0314112A1 Combustor for gas turbine |
05/02/1989 | US4825658 Base metal catalyst |
05/02/1989 | US4825641 Control mechanism for injector diaphragms |
05/02/1989 | US4825640 Combustor with enhanced turbine nozzle cooling |
05/02/1989 | CA1253350A1 Gas turbine engine |
04/26/1989 | EP0312620A1 Combustion air flow rate adjusting device for gas turbine combustor |
04/18/1989 | US4821522 Sealing and cooling arrangement for combustor vane interface |
04/18/1989 | US4821512 Piloting igniter for supersonic combustor |
04/18/1989 | US4821387 Method of manufacturing cooling film devices for combustion chambers of turbomachines |
04/13/1989 | DE3731901A1 Connecting moulded ceramic and metallic components |
04/12/1989 | CN1003879B Cooling scheme for combustor vane interface |
04/11/1989 | US4820097 Fastener with airflow opening |
04/11/1989 | US4819438 Steam cooled rich-burn combustor liner |
04/05/1989 | EP0309485A1 Wide range gaseous fuel combustion system for gas turbine engines. |
04/05/1989 | CN1032230A Gas turbine combustor |
04/04/1989 | US4818218 For attenuating glass fibers |
04/04/1989 | US4817379 Jet propulsion engine and method |
04/04/1989 | US4817378 Gas turbine engine with augmentor and variable area bypass injector |
03/28/1989 | US4815664 Airblast fuel atomizer |
03/28/1989 | US4815283 For a gas turbine engine |
03/22/1989 | CN1031890A Dune-shaped stationary-eddy flameholder |
03/22/1989 | CN1031878A Passively cooled catalytic combustor for stationary combustion turbine |
03/15/1989 | EP0146624B1 Process of intensification of the thermoenergetical cycle and air jet propulsion engines |
03/14/1989 | US4811556 Multiple-propellant air vehicle and propulsion system |
03/09/1989 | WO1989002052A1 Gas turbine combustor |
03/07/1989 | US4810677 Heat-insulating lining for a gas turbine |
03/07/1989 | US4809512 Air-fuel injection system for a turbojet engine |
03/01/1989 | EP0304707A1 Passively cooled catalytic combustor for a stationary combustion turbine |
02/28/1989 | CA1250439A1 Gas turbine engine carburetor |
02/21/1989 | US4805411 For operation with liquid fuelsT?????h)??????????0*0*0*0?0????T |
02/21/1989 | US4805397 Combustion chamber structure for a turbojet engine |
02/09/1989 | WO1989001090A1 Auxiliary combustion chamber for supercharged internal combustion engines |